Fundamentals of spacecraft attitude determination and control

From MaRDI portal
Publication:2251338

DOI10.1007/978-1-4939-0802-8zbMath1381.70006OpenAlexW636927631MaRDI QIDQ2251338

F. Landis Markley, John L. Crassidis

Publication date: 11 July 2014

Published in: Space Technology Library (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/978-1-4939-0802-8




Related Items (27)

State estimation for invariant systems on Lie groups with delayed output measurementsAttitude estimation by multiplicative exogenous Kalman filterError analysis of Davenport's q methodExponential convergence of a nonlinear attitude estimatorTrajectory planning with pose feedback for a dual-arm space robotVelocity-free attitude stabilization with inertial vector measurementsAn improved central difference Kalman filter for satellite attitude estimation with state mutationH inverse optimal attitude tracking on the special orthogonal group SO (3)Bootstrapping globally optimal variational calculus solutionsA robust three-stage central difference Kalman filter for nonlinear discrete-time systems considering faults and unknown inputsDesign and validation of an MPC controller for CMG-based testbedA four-DOF Lagrangian approach to attitude trackingAnalytical quasi-optimal algorithm for the programmed control of the angular motion of a spacecraftA novel stochastically stable variational Bayesian Kalman filter for spacecraft attitude estimationFault modeling of general momentum exchange devices in spacecraft attitude control systemsDecentralized cooperative tracking subject to motion constraintsA bundle framework for observer design on smooth manifolds with symmetryOn the global interpolation of motionAttitude and orbit coupling of planar helio-stable solar sailsOn stability and stabilization of the linearized spacecraft attitude control system with bounded inputsModified Rodrigues parameters: an efficient representation of orientation in 3D vision and graphicsData fusion‐based descriptor approach for attitude estimation under accelerated maneuversAnalytical and iterative solutions to GNSS attitude determination problem in measurement domainFloquet modes and stability analysis of periodic orbit-attitude solutions along Earth-Moon halo orbitsTime integration of rigid bodies modelled with three rotation parametersRobust and fault-tolerant spacecraft attitude control based on an extended-observer designEvent-triggered backstepping control for attitude stabilization of spacecraft


Uses Software





This page was built for publication: Fundamentals of spacecraft attitude determination and control